Accession Number : ADA329728
Title : Recovery of Frozen Flow Losses in Arcjets
Descriptive Note : Final rept.
Corporate Author : OHIO STATE UNIV RESEARCH FOUNDATION COLUMBUS
Personal Author(s) : Subramaniam, V. V.
PDF Url : ADA329728
Report Date : 06 JUN 1996
Pagination or Media Count : 21
Abstract : Our research is concerned with the development of high performance simulations of non-equilibrium flows in arcjets, with the specific aim of identifying and quantifying frozen flow loss mechanisms and channels. Further details of the research can be found in technical articles cited in this report, as well as in several forthcoming papers.
Descriptors : *ARC JET ENGINES, *NONEQUILIBRIUM FLOW, *FROZEN EQUILIBRIUM FLOW, LIQUID PROPELLANT ROCKET ENGINES, SUPERSONIC COMBUSTION, SUPERSONIC FLOW, THRUSTERS, LIQUID ROCKET PROPELLANTS, ELECTRIC PROPULSION, SUPERSONIC NOZZLES, SPECIFIC IMPULSE, THREE DIMENSIONAL FLOW, SPACE PROPULSION.
Subject Categories : Fluid Mechanics
Electric and Ion Propulsion
Distribution Statement : APPROVED FOR PUBLIC RELEASE